Stacking sequence optimizations for composite laminates using fractal branch and bound method: Application for supersonic panel flutter problem with buckling load condition

Author: Hirano Yoshiyasu   Todoroki Akira  

Publisher: Taylor & Francis Ltd

ISSN: 1568-5519

Source: Advanced Composite Materials, Vol.13, Iss.2, 2004-06, pp. : 89-106

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract